Spacecraft relative rotation tracking without angular velocity measurements

Automatica

Volumn 45, Issue 3, 2009, Pages 750-756

  Kristiansen, Raymond ^a   Loría, Antonio ^b   Chaillet, Antoine ^c   Nicklasson, Per Johan ^a  

^a UNIVERSITY OF TROMSØ   (Norway)

^b CNRS   (France)

^c UNIVERSITÉ PARIS SACLAY   (France)

Author keywords

Attitude control; Flight dynamics identification; Output feedback control; Quaternion feedback; Spacecraft formation

Indexed keywords

ANGULAR VELOCITY; ASYMPTOTIC STABILITY; ATTITUDE CONTROL; FEEDBACK CONTROL; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); NAVIGATION; ROTATION; SPACECRAFT; SPACECRAFT PROPULSION; SPATIAL VARIABLES CONTROL; SYSTEM STABILITY; VELOCITY MEASUREMENT;

ANGULAR VELOCITY MEASUREMENTS; BOUNDEDNESS; CLOSED-LOOP SYSTEMS; CONTROLLER STRUCTURES; DIFFERENTIATION FILTERS; INERTIAL FRAMES; LEADER FOLLOWERS; ORBITAL PERTURBATIONS; OUTPUT-FEEDBACK CONTROL; QUATERNION FEEDBACK; RELATIVE ATTITUDES; RELATIVE ROTATIONS; SIMULATION RESULTS; SPACECRAFT FORMATION; STABILITY PROPERTIES;

FEEDBACK;

EID: 60749136497     PISSN: 00051098     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.automatica.2008.10.012     Document Type: Article

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